Noise Studies Of Inlet Guide Vane
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Noise Studies Of Inlet Guide Vane
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Author : John L. Crigler
language : en
Publisher:
Release Date : 1965
Noise Studies Of Inlet Guide Vane written by John L. Crigler and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Airplanes categories.
Turbojet Engine Noise Studies To Evaluate Effects Of Inlet Guide Vane Rotor Spacing
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Author : John L. Crigler
language : en
Publisher:
Release Date : 1968
Turbojet Engine Noise Studies To Evaluate Effects Of Inlet Guide Vane Rotor Spacing written by John L. Crigler and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Airplanes categories.
Noise Reduction By Means Of Inlet Guide Vane Choking In An Axial Flow Compressor
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Author : David Chestnutt
language : en
Publisher:
Release Date : 1968
Noise Reduction By Means Of Inlet Guide Vane Choking In An Axial Flow Compressor written by David Chestnutt and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Airplanes categories.
Effects Of Inlet Guide Vane Configuration And Relative Blade Velocity On Noise From Axial Flow Compressors
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Author : David Chestnutt
language : en
Publisher:
Release Date : 1970
Effects Of Inlet Guide Vane Configuration And Relative Blade Velocity On Noise From Axial Flow Compressors written by David Chestnutt and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Axial flow compressors categories.
Noise Studies Of Inlet Guide Vane
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Author : John L. Crigler
language : en
Publisher:
Release Date : 1965
Noise Studies Of Inlet Guide Vane written by John L. Crigler and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Airplanes categories.
Transonic Compressor Noise
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Author : Aeronautical Research Council (Great Britain)
language : en
Publisher:
Release Date : 1965
Transonic Compressor Noise written by Aeronautical Research Council (Great Britain) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.
Inlet Guide Vane Rotor Stator Interactions For A Single Stage Axial Flow Compressor
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Author : John L. Crigler
language : en
Publisher:
Release Date : 1965
Inlet Guide Vane Rotor Stator Interactions For A Single Stage Axial Flow Compressor written by John L. Crigler and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with NASA technical memorandum categories.
Transonic Compressor Noise
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Author : A. Jean Ross
language : en
Publisher:
Release Date : 1965
Transonic Compressor Noise written by A. Jean Ross and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamic load categories.
Attempts to explain the incremental negative or positive lift induced on an aerofoil by an external non-lifting body (such as an engine nacelle)
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Author :
language : en
Publisher:
Release Date : 1967
written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with categories.
Study And Tests To Reduce Compressor Sounds Of Jet Aircraft
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Author : E. B. Smith
language : en
Publisher:
Release Date : 1968
Study And Tests To Reduce Compressor Sounds Of Jet Aircraft written by E. B. Smith and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Acoustical engineering categories.
Two methods of reducing compressor noise were studied: local sonic velocity regions in inlet guide vanes (or partial choking), and the application of acoustic material to vanes, struts, or duct walls. In the process of the study, some unique facilities for evaluating acoustic material performance for jet engine application were constructed and used, and a large body of data on basic acoustic properties of materials was collected. The performance of acoustic treatment in a duct with air flow was studied, with some major effects identified. An analytical technique has been used to identify the effects on the duct and far field sound pressures produced by lining a duct wall with acoustic material. Noise reduction due to partial choking of inlet guide vanes was demonstrated on both a laboratory test fixture and a full scale engine compressor. Finally, correlation of the duct modes with the blade/vane number was demonstrated in a model compressor. (Author).